Influence of Streamline Adverse Pressure Gradients on the Structure of a Mach 5 Turbulent Boundary Layer (AIAA 2017-1697)
55th AIAA Aerospace Sciences Meeting 2017 ; 2017 ; Grapevine, Texas
2017-01-01
14 pages
Aufsatz (Konferenz)
Englisch
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INFLUENCE OF FAVORABLE PRESSURE GRADIENTS ON A MACH 5.0 TURBULENT BOUNDARY LAYER
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